Single-rotor fixed-wing unmanned aerial vehicle capable of hovering

A fixed-wing and unmanned aerial vehicle technology, applied in the field of single-rotor hovering fixed-wing unmanned aerial vehicle, can solve the problem of low utilization rate

Inactive Publication Date: 2020-05-15
朱治国
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] To this end, the embodiment of the present invention provides a single-rotor hovering fixed-wing unmanned aerial ve

Method used

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  • Single-rotor fixed-wing unmanned aerial vehicle capable of hovering
  • Single-rotor fixed-wing unmanned aerial vehicle capable of hovering
  • Single-rotor fixed-wing unmanned aerial vehicle capable of hovering

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Embodiment Construction

[0052] The implementation mode of the present invention is illustrated by specific specific examples below, and those who are familiar with this technology can easily understand other advantages and effects of the present invention from the contents disclosed in this description. Obviously, the described embodiments are a part of the present invention. , but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0053] A single-rotor hovering fixed-wing unmanned aerial vehicle, such as figure 1 As shown, it includes fuselage 1, wing 2, empennage 3 and propeller 4.

[0054] Such as figure 2 As shown, the empennage 3 has three groups and is connected on the tail side wall of the fuselage 1, and the included angle between any adjacent two groups of empennages 3 is 120 degrees, and each empennage 3 is con...

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Abstract

The embodiment of the invention discloses a single-rotor fixed-wing unmanned aerial vehicle capable of hovering, which comprises a vehicle body, wings, an empennage and a propeller, the propeller is connected to the tail part of the vehicle body, the propeller comprises three sets of blades and a propeller seat connected to the center of each blade, and each blade is hinged with the propeller seat; the main motor is arranged in the machine body, and a rotating shaft of the main motor is connected with the paddle seat; the telescopic part is arranged in the machine body, and the output end achieves the telescopic function; and the three sets of deviation assemblies are connected with the three sets of paddles correspondingly, connected with the output ends of the telescopic parts, driven bythe telescopic parts to deflect and capable of driving the paddles to rotate inwards or outwards. The fixed-wing unmanned aerial vehicle has the technical effects that herringbone take-off and hovering can be achieved, and the utilization rate of all parts of the unmanned aerial vehicle is increased.

Description

technical field [0001] The embodiment of the present invention relates to the technical field of fixed-wing unmanned aerial vehicles, in particular to a single-rotor hoverable fixed-wing unmanned aerial vehicle. Background technique [0002] Fixed-wing UAVs have the advantages of long battery life, large load capacity, and are suitable for long-distance continuous work. Therefore, they are widely used in large-area surveying and mapping and aerial photography. [0003] In the process of large-scale surveying and mapping and aerial photography, fixed-wing UAVs sometimes need to take pictures of a location for a long time. Since the current fixed-wing UAVs cannot hover, they still need to stop when shooting a single location. It is more inconvenient to shoot. The existing vertical lift fixed-wing drones are all multi-rotors, and their multiple rotors are used to perform various functions such as vertical lift and horizontal flight. When vertical lift, some of the rotors will ...

Claims

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Application Information

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IPC IPC(8): B64C27/28B64C27/82
CPCB64C27/28B64C27/82B64C2027/8209
Inventor 朱治国
Owner 朱治国
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